Interference effects in supersonic flow

Interference effects in supersonic flow

A study is made of interference problems with emphasis on low-aspect-ratio supersonic missile configurations. The configurations are composed of slender pointed bodies with circular cross section, plane or cruciform delta wings, and tails which are not specified. For fin-fin interference (no body) g...

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Bibliographic Details
Main Author: Bleviss, Zegmund O.
Format: Others
Published: 1951
Online Access:https://thesis.library.caltech.edu/1002/1/Bleviss_zo_1951.pdf
Bleviss, Zegmund O. (1951) Interference effects in supersonic flow. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/YDMK-MS28. https://resolver.caltech.edu/CaltechETD:etd-03182009-105100 <https://resolver.caltech.edu/CaltechETD:etd-03182009-105100>

Internet

https://thesis.library.caltech.edu/1002/1/Bleviss_zo_1951.pdf
Bleviss, Zegmund O. (1951) Interference effects in supersonic flow. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/YDMK-MS28. https://resolver.caltech.edu/CaltechETD:etd-03182009-105100 <https://resolver.caltech.edu/CaltechETD:etd-03182009-105100>

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